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Sid-Ali Meslioui
Institutions:
United Technologies (Canada),
Pratt and Whitney Canada (Canada)
Observed institutions:
Université de Sherbrooke,
United Technologies (Canada),
Pratt & Whitney (United States),
Pratt and Whitney Canada (Canada)
OpenAlex ID:
A5020967230
Acoustical modeling of micro-perforated panel at high sound pressure levels using equivalent fluid approach
2018
·
Zacharie Laly
, Noureddine Atalla
, et al.
·
Journal of Sound and Vibration
·
56
Evaluation of Acoustic Frequency Methods for the Prediction of Propeller Noise
2019
·
Mark T. Kotwicz Herniczek
, Daniel Feszty
, et al.
·
AIAA Journal
·
33
Sensitivity analysis of micro-perforated panel absorber models at high sound pressure levels
2019
·
Zacharie Laly
, Noureddine Atalla
, et al.
·
Applied Acoustics
·
28
Applicability of Early Acoustic Theory for Modern Propeller Design
2017
·
Mark Kotwicz Herniczek
, Daniel Feszty
, et al.
·
AIAA/CEAS Aeroacoustics Conference
·
20
Comparison of Three Popular Methods for the Prediction of High Speed Propeller Noise
2017
·
Jason Hambrey
, Mark Kotwicz Herniczek
, et al.
·
AIAA/CEAS Aeroacoustics Conference
·
10
Characterization of micro-perforated panel at high sound pressure levels using rigid frame porous models
2017
·
Zacharie Laly
, Noureddine Atalla
, et al.
·
Proceedings of meetings on acoustics
·
6
Modeling of acoustic lined duct with and without grazing air flow by an analytical method
2018
·
Zacharie Laly
, Noureddine Atalla
, et al.
·
Noise Control Engineering Journal
·
4
Acoustic Prediction of High Speed Propeller Noise Using URANS and a Ffowcs Williams-Hawkings Solver
2017
·
Jason Hambrey
, Daniel Feszty
, et al.
·
AIAA Applied Aerodynamics Conference
·
2
Characterization of micro-perforated panel at high sound pressure levels using rigid frame porous models
2017
·
Zacharie Laly
, Noureddine Atalla
, et al.
·
The Journal of the Acoustical Society of America
·
2
Source Identification of a Gas Turbine Engine Using an Inverse Method With Beamforming
2012
·
Iman Khatami
, Alain Berry
, et al.
·
1
Analytical formulation of the radiation of sound from a rectangular lined duct
1998
·
Sid-Ali Meslioui
·
Canadian acoustics
·
1
Jet noise prediction model for turbofan engines with internal forced mixers
2007
·
Sid-Ali Meslioui
·
Canadian acoustics
PDF
Determination of CFD Turbulence Scales for Lobed Mixer Jet Noise Prediction
2007
·
Sid-Ali Meslioui
, Mark Cunningham
, et al.
·
ASME Turbo Expo: Turbomachinery Technical Conference and Exposition (GT)
Duct Modes Conversion Due to the Presence of Liners
2002
·
Sid-Ali Meslioui
·
Canadian acoustics
PDF
Broadband acoustic absorber panel
1999
·
Sid-Ali Meslioui
·
Canadian acoustics
PDF
Experimental study of the sound reduction for the side air-intake of a helicopter turboshaft engine
1997
·
Sid-Ali Meslioui
·
Canadian acoustics
PDF
Contribution a l'etude de l'insonorisation des entrees d'air laterales de turbomoteurs d'helicopteres
1996
·
Sid-Ali Meslioui
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Works count:
17
Citation count:
163
H-index:
6
I10-index:
5
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